发明名称 |
Coated high temperature combustor liner |
摘要 |
Each panel of the louver liner of the combustor of a gas turbine engine is coated with a ceramic composition on the surface adjacent the combustion zone with a tapered end at the lip of the cooling air film generating mechanism. A second taper may be incorporated at the back side of the lip of the next adjacent cooling air film generating mechanism.
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申请公布号 |
US4655044(A) |
申请公布日期 |
1987.04.07 |
申请号 |
US19830563848 |
申请日期 |
1983.12.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DIERBERGER, JAMES A.;TUMICKI, THOMAS F. |
分类号 |
F23R3/08;F23R3/00;F23R3/06;F23R3/42;(IPC1-7):F02C1/00;F02G3/00 |
主分类号 |
F23R3/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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